Thermal modal analysis of hypersonic composite wing on transient aerodynamic heating

Thermal modal analysis of hypersonic composite wing on transient aerodynamic heating

Abstract Considering the influence of thermal stress and material property variations, this study employs the Navier–Stokes equations and Fourier heat conduction law to establish a semi-implicit time-domain numerical analysis method for hypersonic aerothermal-structural coupling. Study the temporal...

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Bibliographic Details
Main Authors: Kangjie Wang, Junli Wang, Zhiyuan Liu, Sheng Zhang, Baosheng Zhang, Wenyong Quan
Format: Article
Language:English
Published: Nature Portfolio 2024-05-01
Series:Scientific Reports
Subjects:
Hypersonic
Composite wing
Aerodynamic heating
CFD/CSD
Online Access:https://doi.org/10.1038/s41598-024-61900-y

Internet

https://doi.org/10.1038/s41598-024-61900-y

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